• DocumentCode
    1528473
  • Title

    Stability of a DC SF6 arc in an axially accelerating flow

  • Author

    Blundell, R.E. ; Fang, Michael T C ; Vourdas, A.

  • Author_Institution
    Dept. of Electr. Eng. & Electron., Liverpool Univ., UK
  • Volume
    25
  • Issue
    5
  • fYear
    1997
  • fDate
    10/1/1997 12:00:00 AM
  • Firstpage
    852
  • Lastpage
    859
  • Abstract
    The stability of a DC arc burning in an axially accelerating flow of SF6 is investigated. The method of normal modes is applied to the equations governing an axisymmetric, infinitesimal perturbation of a self-similar arc, and solutions are obtained numerically. Results are presented for a range of discharge conditions. The physical mechanisms causing instability are deduced from equations for the time-averaged, squared enthalpy, and velocity of a perturbation. The steep radial gradient of the density at the edge of the arc is shown to cause instability. The effect of density fluctuations in comparison with velocity fluctuations is not negligible, and the possible implication of this result for turbulent arc modeling is discussed
  • Keywords
    arcs (electric); plasma density; plasma devices; plasma flow; plasma fluctuations; plasma instability; plasma thermodynamics; plasma turbulence; sulphur compounds; DC arc burning; SF6; SF6 arc; axially accelerating flow; axisymmetric infinitesimal perturbation; density; density fluctuations; discharge conditions; instability; normal modes; perturbation velocity; physical mechanisms; self-similar arc; stability; steep radial gradient; time-averaged, squared enthalpy; turbulent arc modeling; velocity fluctuations; Acceleration; Circuit breakers; Circuit stability; Fluctuations; Heat engines; Nonlinear equations; Plasma devices; Plasma stability; Predictive models; Stability analysis;
  • fLanguage
    English
  • Journal_Title
    Plasma Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0093-3813
  • Type

    jour

  • DOI
    10.1109/27.649580
  • Filename
    649580